US6924185B2 - Fuse structure and method to form the same - Google Patents
Fuse structure and method to form the same Download PDFInfo
- Publication number
- US6924185B2 US6924185B2 US10/680,618 US68061803A US6924185B2 US 6924185 B2 US6924185 B2 US 6924185B2 US 68061803 A US68061803 A US 68061803A US 6924185 B2 US6924185 B2 US 6924185B2
- Authority
- US
- United States
- Prior art keywords
- fuse
- layer
- insulator layer
- insulator
- electrodes
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L23/00—Details of semiconductor or other solid state devices
- H01L23/52—Arrangements for conducting electric current within the device in operation from one component to another, i.e. interconnections, e.g. wires, lead frames
- H01L23/522—Arrangements for conducting electric current within the device in operation from one component to another, i.e. interconnections, e.g. wires, lead frames including external interconnections consisting of a multilayer structure of conductive and insulating layers inseparably formed on the semiconductor body
- H01L23/525—Arrangements for conducting electric current within the device in operation from one component to another, i.e. interconnections, e.g. wires, lead frames including external interconnections consisting of a multilayer structure of conductive and insulating layers inseparably formed on the semiconductor body with adaptable interconnections
- H01L23/5256—Arrangements for conducting electric current within the device in operation from one component to another, i.e. interconnections, e.g. wires, lead frames including external interconnections consisting of a multilayer structure of conductive and insulating layers inseparably formed on the semiconductor body with adaptable interconnections comprising fuses, i.e. connections having their state changed from conductive to non-conductive
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L2924/00—Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
- H01L2924/0001—Technical content checked by a classifier
- H01L2924/0002—Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
Definitions
- the present invention generally relates to fuses included within semiconductor structures which protect semiconductor devices from excessive voltage and/or current or which selectively and permanently connect/disconnect semiconductor devices from one another.
- fuse structures that are made out of existing doped polysilicon layers that are typically patterned to define transistor gates over a semiconductor structure.
- the fuse structure may be “programmed” by passing a sufficiently high current that melts and vaporizes a portion of the polysilicon fuse.
- the fuse structure In the programmed state, the fuse structure typically has a resistance that is substantially greater than the non-programmed state, thereby producing an open circuit. This is of course counter to antifuse devices that become short circuits (i.e., substantially decreased resistance) in a programmed state.
- traditional fuse structures work well, they typically consume a large amount of power in programming that may make them unfit for a variety of low power integrated circuit products.
- fuses are made in semiconductors within the chip.
- the prior art is bereft of devices in which fuses are plated at the uppermost level.
- the prior art is devoid of devices in which a damascene process is used to form the fuse structure at the uppermost level. Because softer and inherently weaker materials that will pass oxygen through them are beginning to be used by designers and manufacturers, there is a need to create easily fabricated fuses that will not damage the product when they are blown.
- the present invention has been devised, and it is an object of the present invention to provide a structure and method for a plated fuse structure, which will not damage the product they are configured for, when the fuse is blown.
- a method and structure for a fuse structure comprising an insulator layer, a plurality of fuse electrodes extending through the insulator layer to an underlying wiring layer, an electroplated fuse element connected to the electrodes, and an interface wall, wherein the fuse element is positioned external to the insulator, with a gap juxtaposed between the insulator and the fuse element.
- the interface wall further comprises a first side wall, a second side wall, and an inner wall, wherein the inner wall is disposed within the gap.
- the fuse electrodes are diametrically opposed to one another and the fuse elements are perpendicularly disposed above the plurality of fuse electrodes.
- the fuse By plating a material, such as nickel, the fuse can be exposed to air. Nickel is self-passivating and thereby it is also a good oxygen barrier.
- the steps of forming the vias and troughs (fuse) in an insulator are deposition followed by a lithography/etching process to form the vias and the troughs.
- deposition of liner/barrier/seed by depositing a suitable material i.e., nickel
- a chemical mechanical-polish is performed.
- Prior art for the back end of the line fuses do not accommodate low modulus materials being used as an interlevel dielectric below the fuse. When the fuse is blown, damage occurs and can cause the chip to become nonfunctional.
- Current fuses are made of aluminum which is formed by using a rie process. The aluminum is a blanket deposited and etched off in the areas that it is not desired. This also means that if there is any nonuniformity in the metal deposition, it will remain there, causing a differential in the power needed to blow the fuses across the substrate.
- the current thickness of the aluminum is also problematic, wherein the thickness gives rise to the chance of extraneous aluminum being displaced onto nearby structures thereby causing a short.
- the present invention is thinner, and therefore, there is less material to be displaced.
- FIG. 1 is a cross-sectional schematic diagram of a fuse structure according to the present invention
- FIG. 2 is a cross-sectional schematic diagram of a fuse structure according to the present invention.
- FIG. 3 is a cross-sectional schematic diagram of a fuse structure according to the present invention.
- FIG. 4 is a cross-sectional schematic diagram of a fuse structure according to the present invention.
- FIG. 5 is a cross-sectional schematic diagram of a fuse structure according to the present invention.
- FIG. 6 is a cross-sectional schematic diagram of a fuse structure according to the present invention.
- FIG. 7 is a flow diagram of a preferred method of the present invention.
- FIG. 1 there are shown preferred embodiments of the method and structure according to the present invention. Referring to FIGS. 1-7 , a first embodiment of the present invention will be described below.
- the present invention pertains to a fuse, which is a plated structure that is fabricated in a damascene fashion.
- the present process provides for electroplating. Additionally, an electroless plating with materials such as NiP could be used, as would be common knowledge for those skilled in the art.
- the insulating material can be etched away from the section of the fuse that needs to be blown. This will decrease the amount of damage that the final passivation layer (insulator layer) will receive.
- the fuse can be made very thin compared to current fuses.
- the thickness will be determined by the skill level of the fabricators in the area of CMP (chemical mechanical polish). Fuses of aluminum are currently greater than 1 ⁇ m thick. Thinner metal structures can be made with damascene processing. Currently, metal levels that are 0.2 ⁇ m thick can be made. Because there is less material to blow, the forces associated with that action can be reduced. Then, by using a resilient metal such as nickel, there is the option of etching the insulator after the chemical mechanical polish and not etching the fuse; the fuse acts as a mask. This allows the fuse to be physically residing above the insulator and helps inhibit the transfer of energy from the fuse blow.
- nickel may be used as the electroplating material, but many metals can be used that are common with electroplating. Nickel offers a metal that can, be electroplated, easily polished, is self passivating and can be fabricated simultaneously during another process. There are several options for the material to be used other than nickel, such as aluminum, tungsten, gold, or copper.
- FIG. 1 there is shown a fuse structure 100 comprising a wiring layer 110 further comprising a plurality of wire elements 120 interspersed therein.
- a final passivation layer (insulator layer) 115 is shown on top of the wiring layer 110 .
- a fuse portion 130 of the fuse structure 100 is shown as an inverted U-shaped device. However, those skilled in the art will recognize that any geometric configuration may be used for the fuse portion 130 .
- the fuse portion 130 further comprises a generally horizontal electroplated fuse element 140 , with a pair of fuse electrodes 150 , 151 extending downwardly therefrom. The fuse electrodes 150 , 151 contact the plurality of wire elements 120 in the wiring layer 110 of the fuse structure 100 .
- an air gap 160 is shown juxtaposed between the fuse element 140 and the top of the passivation layer (insulator layer) 115 .
- the air gap 160 is open from the front and rear sides, as opposed to being sealed.
- the fuse element 130 contacts the wire elements 120 through the pair of fuse electrodes 150 and 151 .
- the fuse element 130 itself, is not in contact with the underlying structure. This allows all surfaces of the fuse element to be plated.
- FIG. 2 illustrates the final passivation layer 115 more thoroughly.
- the final passivation layer 115 comprises a top layer 200 , a middle layer 210 , and a bottom layer 220 .
- the top layer 200 can be any thickness and preferably comprises 3.5 kilo angstroms of silicon dioxide.
- the middle layer 210 preferably comprises 4.0 kilo angstroms of silicon nitride.
- the bottom layer 220 preferably comprises 4.5 kilo angstroms of silicon dioxide.
- FIG. 3 shows the fuse structure 100 undergoing a damascene process.
- a plurality of voids 300 , 301 are made in the insulator layer 115 using any well-known technique such as lithographic patterning.
- the top layer 200 of the insulator layer 115 is further reduced in height 205 in the portion of the insulator layer 115 disposed in between the voids 300 , 301 .
- the height difference is created by utilizing lithography and etch.
- the first lithography/etch forms the vias, and a second lithography/etch forms the fuse.
- the etch is different for each of the features, but this would be common knowledge for anyone skilled in the art.
- Voids 300 and 301 are formed at the same time and the reduction in height 205 is formed at a different time (the decision to form the vias first or the fuse first is discretionary). If there is insufficient skill to etch top layer 200 partially, one could make top layer 200 the desired thickness of the fuse and use the middle layer 210 as an etch stop. This would mean that a selective etch would be required which is not uncommon in the industry.
- the fuse/electrode material 130 of the fuse structure 100 is shown to fill the voids 300 , 301 .
- the fuse/electrodes 150 , 151 fill the voids 300 , 301 , and the fuse element 140 rests atop the top layer 200 of the insulator layer 115 , whereby the fuse element 140 is flush with the top layer 200 of the insulator layer 115 located on the sides of the fuse structure 100 , and the height-reduced insulator layer 205 is between the underside of the fuse element 140 and the upper portion of the middle layer 210 of the insulator layer 115 .
- the material selected for the fuse electrode material 130 may be nickel, gold, etc. . . .
- the fuse/electrode material 130 can be deposited using any conventional damascene process, such as chemical vapor deposition (CVD), liquid phase deposition, and ion physical vapor deposition (IPVD), etc.
- CVD chemical vapor deposition
- IPVD ion physical vapor deposition
- FIG. 5 shows the fuse structure 100 undergoing an etching process, whereby the top layer 200 of the insulator layer 115 is removed.
- the height-reduced insulator layer 205 is simultaneously removed during this etching (for example, a wet etch). This removal of the top layer 200 , and the height-reduced insulator layer 205 creates an open air gap 160 between the fuse element 140 and the middle layer 210 of the insulator layer 210 .
- the etching allows the fuse portion 130 to protrude from the insulator layer 115 , whereby the fuse element 140 is no longer flush with the insulator layer 115 .
- the fuse structure 100 is shown with a plurality of PSPI (photosensitive polyimide) walls 600 , 601 , and a residual PSPI wall 620 disposed within the air gap 160 .
- PSPI photosensitive polyimide
- the residual PSPI wall 620 does not completely fill the air gap 160 .
- an air gap 160 still remains intact.
- PSPI is made in different tones.
- the PSPI is coated on the substrate much the same way as the photoresist is applied. The only difference is that the PSPI is usually a much more viscous polymer.
- the PSPI is “soft baked” on a hot plate, which is well known in the art.
- the PSPI is then exposed in lithography using normal lithographic techniques.
- the PSPI is then developed, which means for the positive tone, the PSPI will remain on the substrate any place that the light does not expose the PSPI.
- the first embodiment for the formation of the reduction of height 205 in FIG. 3 comes into force here.
- a selective etch can be used to undercut the fuse. This means that the silicon dioxide will be removed from under the fuse.
- This fuse width is in the order of 0.5 ⁇ m, this dimension lends itself to making the undercut easier.
- the limit of the ability of the etch to undercut the structure is determined by the abilities of the fabricators skilled in the art.
- the fuse acts as a mask allowing the PSPI to remain under the fuse. This may act as a cushion when the fuse blow takes place.
- FIG. 7 details the method in which the fuse structure is produced.
- an insulator layer 1 15 is applied 700 on top of a wiring layer 110 .
- voids 300 , 301 are created 710 in the insulator layer 115 and the height of area 205 is reduced.
- the voids 300 , 301 are filled 720 with an electroplated fuse portion 130 .
- the upper layer 200 of the insulator layer 115 is etched 730 . This forms 740 a gap 160 between the electroplated fuse portion 130 and the insulator layer 115 .
- a plurality of interface walls 600 , 601 , 620 are disposed 750 on the insulator layer 115 .
- the final passivation layer is left without the top layer 200 .
- the fuse element 140 in FIG. 1 is formed in the middle layer 210 of FIG. 2 . This makes the formation of the air gap 160 very difficult to fabricate.
- the benefits are that there are less processing steps to form the structure, which uses the thickness of the fuse as the singular more important item in the alleviation of fuseblow induced damage.
- the depth of the fuse section that is to be blown may be as thin as a metal deposition tool can cover a two level structure. That is, the metal can be thinned to the point until it becomes non-continuous. This allows the fuse to be blown with the lower power required in today's advanced electronics. For example, if a conventional damascene process is used to form the electrode/fuse material 130 (e.g., forming layers of 100 angstroms of TaN and 100 angstroms of Ta) the resulting fuse could be as thin as 200 angstroms.
- the present invention is unique in that a seed material must be deposited (i.e., IPVD copper, sputtered nickel, electroless NiP, W, etc.).
- IPVD copper, sputtered nickel, electroless NiP, W, etc. The thickness of these materials requires only that the material remain continuous. For example, thicknesses of 100-350 angstroms have been achieved.
- the electroplated material is deposited, such as Ni, NiP, or any conductor that will plate off the seeds that are to be used. Electroplating and electroless plating are well-known processes and thoroughly documented. After the plating, the substrate is polished (CMP) to make all the fuses uniform.
- fuse electrodes 150 and 151 are formed and then, a thick (greater than 1 ⁇ m) aluminum layer is deposited. Lithography leaves photoresist on all the areas that are needed to remain on the substrate. The substrate is then etched to remove the unwanted aluminum leaving the fuse on the top. The fuse that is made is very thick and the uniformity is dependent on the ability of the aluminum deposition tooling capabilities.
- the present invention cannot be used for antifuse devices because antifuses deal with breaking down a dielectric to form a connection. Whereas in the present invention, there is an opening in a conductor to prevent continuity.
- the process for electroplating begins by first starting the electroplating process with the structure shown in FIG. 2 .
- a line/barrier/seed is deposited.
- the substrate is electroplated; and fourth, a CMP is performed to planarize the substrate and polish off the plated material between structures. If electroless plating is used, then step 3 would be an electroless activation layer (i.e. Pd for NiP) deposition followed by electroless plating.
- An alternate embodiment involves the use of other deposited conductors.
- liner materials for the fuse could be used. If a material such as TaN is used, then depositing as little as the material would allow to become a hermetic seal for the level below would be utilized. As such, 350 angstroms would be sufficient for this requirement.
- Other materials could be W, Ti, Ta, Sn, TiW, etc.
- the depth of the level 310 in FIG. 3 would be dependant on the abilities of the CMP process. If the process lends itself to dishing, a deeper level 310 would be needed. Dishing refers to the flexing of a pad during the CMP process and removing material that was meant to remain. For the normal polishing techniques that are used, level 310 could be as shallow as 200 angstroms. Other fabricators would need to determine the abilities of their polishing process to determine the depth requirement.
- the advantage of using a material like TaN is that it can be used as a mask even if it is very thin (less than 1,000 angstroms). This would allow the ability to form the air gap 160 with an ultra-thin fuse.
- the present invention provides for the following three processes. First, for an electroplated fuse, beginning with the structure shown in FIG. 3 , a liner/barrier/seed is applied. After electroplating, a CMP is performed. Then, the PSPI is applied, and a lithography is performed and developed. Lastly, a PSPI cure is performed. Secondly, for an electroless plating fuse, the process begins with the structure shown in FIG. 3 . Then a liner/barrier/seed is applied. Next, an activation layer electroless plate is deposited. After performing a CMU the structure is etched. Next, the PSPI is applied, and a lithography is performed and developed followed by a curing process.
- the process begins with the structure shown in FIG. 3 .
- a liner/barrier fuse material
- the structure is etched.
- the PSPI is applied, and a lithography is performed and developed followed by a curing process.
- the first two processes allow the fabricator to build other structures at the same time with the same materials. This makes the process more manufacturable and more cost effective.
- the last option applies if the fabricator needed the thinnest possible fuse, which would probably be for a very high-end application, where the cost is offset by the need for effect performance of the fuse and an ability to blow it with very low power.
Landscapes
- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Design And Manufacture Of Integrated Circuits (AREA)
- Internal Circuitry In Semiconductor Integrated Circuit Devices (AREA)
- Fuses (AREA)
Abstract
A method and structure for a fuse structure comprises an insulator layer, a plurality of fuse electrodes extending through the insulator layer to an underlying wiring layer, an electroplated fuse element connected to the electrodes, and an interface wall. The fuse element is positioned external to the insulator, with a gap juxtaposed between the insulator and the fuse element. The interface wall further comprises a first side wall, a second side wall, and an inner wall, wherein the inner wall is disposed within the gap. The fuse electrodes are diametrically opposed to one another, and the fuse element is perpendicularly disposed above the fuse electrodes. The fuse element is either electroplatted, electroless plated, or is an ultra thin fuse.
Description
This application is a division of U.S. application Ser. No. 09/992,344 filed Nov. 14, 2001.
1. Field of the Invention
The present invention generally relates to fuses included within semiconductor structures which protect semiconductor devices from excessive voltage and/or current or which selectively and permanently connect/disconnect semiconductor devices from one another.
2. Description of the Related Art
As the size and voltage/current ratings of semiconductor devices becomes smaller, as a result of device miniaturization, the fuses which protect or disconnect such devices must be opened (“blown”) with smaller amounts of energy to accommodate the delicacy of todays semiconductor products. In an effort to reduce and/or eliminate the damage caused to the product when the fuses are blown, designers have been patterning fuses in various manners to solve this problem and to reduce costs as well.
There are several kinds of integrated circuit applications that require some form of electrically programmable memory for storing information. The information stored varies significantly in size ranging from a few bits used to program simple identification data, to several megabits used to program computer programs. Fabricating these types of memory devices along with core logic integrated circuitry adds a number of additional processing steps that significantly raise product costs. Usually, the additional product costs are difficult to justify when only relatively small amounts of electrically programmable elements are needed for a particular integrated circuit application.
As such, in order to reduce costs, semiconductor designers have been implementing “fuse” structures that are made out of existing doped polysilicon layers that are typically patterned to define transistor gates over a semiconductor structure. Once formed, the fuse structure may be “programmed” by passing a sufficiently high current that melts and vaporizes a portion of the polysilicon fuse. In the programmed state, the fuse structure typically has a resistance that is substantially greater than the non-programmed state, thereby producing an open circuit. This is of course counter to antifuse devices that become short circuits (i.e., substantially decreased resistance) in a programmed state. Although traditional fuse structures work well, they typically consume a large amount of power in programming that may make them unfit for a variety of low power integrated circuit products.
Current back end fuses are made of aluminum or copper and formerly were made of tungsten. Polysilicon is used in the front end of the chip which can tolerate high temperatures (this is the device end not the interconnect end).
Currently, fuses are made in semiconductors within the chip. However, the prior art is bereft of devices in which fuses are plated at the uppermost level. Moreover, the prior art is devoid of devices in which a damascene process is used to form the fuse structure at the uppermost level. Because softer and inherently weaker materials that will pass oxygen through them are beginning to be used by designers and manufacturers, there is a need to create easily fabricated fuses that will not damage the product when they are blown.
In view of the foregoing and other problems, disadvantages, and drawbacks of the conventional fuse structures the present invention has been devised, and it is an object of the present invention to provide a structure and method for a plated fuse structure, which will not damage the product they are configured for, when the fuse is blown.
In order to attain the object suggested above, there is provided, according to one aspect of the invention a method and structure for a fuse structure comprising an insulator layer, a plurality of fuse electrodes extending through the insulator layer to an underlying wiring layer, an electroplated fuse element connected to the electrodes, and an interface wall, wherein the fuse element is positioned external to the insulator, with a gap juxtaposed between the insulator and the fuse element. The interface wall further comprises a first side wall, a second side wall, and an inner wall, wherein the inner wall is disposed within the gap. The fuse electrodes are diametrically opposed to one another and the fuse elements are perpendicularly disposed above the plurality of fuse electrodes.
By plating a material, such as nickel, the fuse can be exposed to air. Nickel is self-passivating and thereby it is also a good oxygen barrier. The steps of forming the vias and troughs (fuse) in an insulator are deposition followed by a lithography/etching process to form the vias and the troughs. Next, deposition of liner/barrier/seed by depositing a suitable material (i.e., nickel) occurs, and lastly, a chemical mechanical-polish is performed.
These steps should be familiar to anyone who is skilled in the art. Prior art for the back end of the line fuses do not accommodate low modulus materials being used as an interlevel dielectric below the fuse. When the fuse is blown, damage occurs and can cause the chip to become nonfunctional. Current fuses are made of aluminum which is formed by using a rie process. The aluminum is a blanket deposited and etched off in the areas that it is not desired. This also means that if there is any nonuniformity in the metal deposition, it will remain there, causing a differential in the power needed to blow the fuses across the substrate. The current thickness of the aluminum is also problematic, wherein the thickness gives rise to the chance of extraneous aluminum being displaced onto nearby structures thereby causing a short. The present invention is thinner, and therefore, there is less material to be displaced.
The foregoing and other objects, aspects and advantages will be better understood from the following detailed description of a preferred embodiment of the invention with reference to the drawings, in which:
Referring now to the drawings, and more particularly to FIG. 1 , there are shown preferred embodiments of the method and structure according to the present invention. Referring to FIGS. 1-7 , a first embodiment of the present invention will be described below.
The present invention pertains to a fuse, which is a plated structure that is fabricated in a damascene fashion.
The present process provides for electroplating. Additionally, an electroless plating with materials such as NiP could be used, as would be common knowledge for those skilled in the art.
Depending on the material that is chosen to plate the fuse structure with, the insulating material can be etched away from the section of the fuse that needs to be blown. This will decrease the amount of damage that the final passivation layer (insulator layer) will receive.
The damage is decreased in two ways. First, by using a damascene process, the fuse can be made very thin compared to current fuses. The thickness will be determined by the skill level of the fabricators in the area of CMP (chemical mechanical polish). Fuses of aluminum are currently greater than 1 μm thick. Thinner metal structures can be made with damascene processing. Currently, metal levels that are 0.2 μm thick can be made. Because there is less material to blow, the forces associated with that action can be reduced. Then, by using a resilient metal such as nickel, there is the option of etching the insulator after the chemical mechanical polish and not etching the fuse; the fuse acts as a mask. This allows the fuse to be physically residing above the insulator and helps inhibit the transfer of energy from the fuse blow.
In the current disclosure nickel may be used as the electroplating material, but many metals can be used that are common with electroplating. Nickel offers a metal that can, be electroplated, easily polished, is self passivating and can be fabricated simultaneously during another process. There are several options for the material to be used other than nickel, such as aluminum, tungsten, gold, or copper.
In FIG. 1 , there is shown a fuse structure 100 comprising a wiring layer 110 further comprising a plurality of wire elements 120 interspersed therein. A final passivation layer (insulator layer) 115 is shown on top of the wiring layer 110. A fuse portion 130 of the fuse structure 100 is shown as an inverted U-shaped device. However, those skilled in the art will recognize that any geometric configuration may be used for the fuse portion 130. The fuse portion 130 further comprises a generally horizontal electroplated fuse element 140, with a pair of fuse electrodes 150, 151 extending downwardly therefrom. The fuse electrodes 150, 151 contact the plurality of wire elements 120 in the wiring layer 110 of the fuse structure 100. Finally, an air gap 160 is shown juxtaposed between the fuse element 140 and the top of the passivation layer (insulator layer) 115. The air gap 160 is open from the front and rear sides, as opposed to being sealed. Further, the fuse element 130 contacts the wire elements 120 through the pair of fuse electrodes 150 and 151. However, the fuse element 130, itself, is not in contact with the underlying structure. This allows all surfaces of the fuse element to be plated.
In FIG. 4 , the fuse/electrode material 130 of the fuse structure 100 is shown to fill the voids 300, 301. The fuse/ electrodes 150, 151 fill the voids 300, 301, and the fuse element 140 rests atop the top layer 200 of the insulator layer 115, whereby the fuse element 140 is flush with the top layer 200 of the insulator layer 115 located on the sides of the fuse structure 100, and the height-reduced insulator layer 205 is between the underside of the fuse element 140 and the upper portion of the middle layer 210 of the insulator layer 115. The material selected for the fuse electrode material 130 may be nickel, gold, etc. . . . , or any similar material capable of being electroplated in a similar fashion. The fuse/electrode material 130 can be deposited using any conventional damascene process, such as chemical vapor deposition (CVD), liquid phase deposition, and ion physical vapor deposition (IPVD), etc.
Next, as shown in FIG. 6 , the fuse structure 100 is shown with a plurality of PSPI (photosensitive polyimide) walls 600, 601, and a residual PSPI wall 620 disposed within the air gap 160. However, the residual PSPI wall 620 does not completely fill the air gap 160. Thus, an air gap 160 still remains intact. PSPI is made in different tones. The PSPI is coated on the substrate much the same way as the photoresist is applied. The only difference is that the PSPI is usually a much more viscous polymer. After the application, the PSPI is “soft baked” on a hot plate, which is well known in the art. The PSPI is then exposed in lithography using normal lithographic techniques. The PSPI is then developed, which means for the positive tone, the PSPI will remain on the substrate any place that the light does not expose the PSPI.
For more advanced reactive ion etching capabilities, the first embodiment for the formation of the reduction of height 205 in FIG. 3 comes into force here. After the fuse is metalized a selective etch can be used to undercut the fuse. This means that the silicon dioxide will be removed from under the fuse. This fuse width is in the order of 0.5 μm, this dimension lends itself to making the undercut easier. The limit of the ability of the etch to undercut the structure is determined by the abilities of the fabricators skilled in the art.
Since the fuse shadows some of the PSPI that will flow under it in the air gap 160 in FIG. 1 , the fuse acts as a mask allowing the PSPI to remain under the fuse. This may act as a cushion when the fuse blow takes place.
In a second embodiment, the final passivation layer is left without the top layer 200. The fuse element 140 in FIG. 1 is formed in the middle layer 210 of FIG. 2. This makes the formation of the air gap 160 very difficult to fabricate. However, the benefits are that there are less processing steps to form the structure, which uses the thickness of the fuse as the singular more important item in the alleviation of fuseblow induced damage.
Here, the ability to make the fuse very thin is available since a damascene process is being used. The depth of the fuse section that is to be blown may be as thin as a metal deposition tool can cover a two level structure. That is, the metal can be thinned to the point until it becomes non-continuous. This allows the fuse to be blown with the lower power required in today's advanced electronics. For example, if a conventional damascene process is used to form the electrode/fuse material 130 (e.g., forming layers of 100 angstroms of TaN and 100 angstroms of Ta) the resulting fuse could be as thin as 200 angstroms.
The present invention is unique in that a seed material must be deposited (i.e., IPVD copper, sputtered nickel, electroless NiP, W, etc.). The thickness of these materials requires only that the material remain continuous. For example, thicknesses of 100-350 angstroms have been achieved. Then, the electroplated material is deposited, such as Ni, NiP, or any conductor that will plate off the seeds that are to be used. Electroplating and electroless plating are well-known processes and thoroughly documented. After the plating, the substrate is polished (CMP) to make all the fuses uniform.
Currently, fuse electrodes 150 and 151 are formed and then, a thick (greater than 1 μm) aluminum layer is deposited. Lithography leaves photoresist on all the areas that are needed to remain on the substrate. The substrate is then etched to remove the unwanted aluminum leaving the fuse on the top. The fuse that is made is very thick and the uniformity is dependent on the ability of the aluminum deposition tooling capabilities.
The present invention cannot be used for antifuse devices because antifuses deal with breaking down a dielectric to form a connection. Whereas in the present invention, there is an opening in a conductor to prevent continuity.
The process for electroplating begins by first starting the electroplating process with the structure shown in FIG. 2. Next, a line/barrier/seed is deposited. Third, the substrate is electroplated; and fourth, a CMP is performed to planarize the substrate and polish off the plated material between structures. If electroless plating is used, then step 3 would be an electroless activation layer (i.e. Pd for NiP) deposition followed by electroless plating.
An alternate embodiment involves the use of other deposited conductors. For example, liner materials for the fuse could be used. If a material such as TaN is used, then depositing as little as the material would allow to become a hermetic seal for the level below would be utilized. As such, 350 angstroms would be sufficient for this requirement. Other materials could be W, Ti, Ta, Sn, TiW, etc.
The depth of the level 310 in FIG. 3 would be dependant on the abilities of the CMP process. If the process lends itself to dishing, a deeper level 310 would be needed. Dishing refers to the flexing of a pad during the CMP process and removing material that was meant to remain. For the normal polishing techniques that are used, level 310 could be as shallow as 200 angstroms. Other fabricators would need to determine the abilities of their polishing process to determine the depth requirement.
The advantage of using a material like TaN is that it can be used as a mask even if it is very thin (less than 1,000 angstroms). This would allow the ability to form the air gap 160 with an ultra-thin fuse.
Summarily, the present invention provides for the following three processes. First, for an electroplated fuse, beginning with the structure shown in FIG. 3 , a liner/barrier/seed is applied. After electroplating, a CMP is performed. Then, the PSPI is applied, and a lithography is performed and developed. Lastly, a PSPI cure is performed. Secondly, for an electroless plating fuse, the process begins with the structure shown in FIG. 3. Then a liner/barrier/seed is applied. Next, an activation layer electroless plate is deposited. After performing a CMU the structure is etched. Next, the PSPI is applied, and a lithography is performed and developed followed by a curing process. Lastly, for an ultra thin fuse, the process begins with the structure shown in FIG. 3. Next, a liner/barrier (fuse material) is applied. After performing a CMP the structure is etched. Next, the PSPI is applied, and a lithography is performed and developed followed by a curing process.
The first two processes allow the fabricator to build other structures at the same time with the same materials. This makes the process more manufacturable and more cost effective. The last option applies if the fabricator needed the thinnest possible fuse, which would probably be for a very high-end application, where the cost is offset by the need for effect performance of the fuse and an ability to blow it with very low power.
While the invention has been described in terms of preferred embodiments, those skilled in the art will recognize that the invention can be practiced with modification within the spirit and scope of the appended claims.
Claims (9)
1. A method of producing a fuse structure, said method comprising:
applying an insulator layer over a wiring layer; wherein said insulator layer comprises an upper layer, a middle layer, and a bottom layer;
creating voids in said insulating layer and reducing a height of a fuse area of said upper layer betwee said voids; filling said voids and said fuse with a fuse material to form fuse electrodes in said voids and a fuse element above said fuse area;
removing said upper layer of said insulator layer, wherein said removing forms a gap between said fuse element and said insulator layer;
electroplating said fuse element; and
applying an upper interface wall on said insulator layer.
2. The method of claim 1 , wherein said upper layer and said bottom layer of said insulator layer comprise silicon dioxide.
3. The method of claim 1 , wherein said middle layer of said insulator layer comprises silicon nitride.
4. The method of claim 1 , wherein said step of creating voids in said insulator layer further comprises creating a plurality of voids from the upper layer of the insulator layer to an upper portion of the wiring layer.
5. The method of claim 1 , wherein said fuse electrodes extend through said insulator layer to an underlying wiring layer.
6. The method of claim 5 , wherein said fuse electrodes are diametrically opposed to one another.
7. The method in claim 5 , wherein said fuse element is perpendicularly disposed above said fuse electrodes.
8. The method of claim 1 , wherein said gap is confined by said fuse electrodes, said fuse element, and said middle layer of said insulator layer.
9. The method of claim 1 , wherein said upper interface wall further comprises a first side wall, a second side wall, and an inner wall, wherein said inner wall is disposed within said gap.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/680,618 US6924185B2 (en) | 2001-11-14 | 2003-10-07 | Fuse structure and method to form the same |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/992,344 US6927472B2 (en) | 2001-11-14 | 2001-11-14 | Fuse structure and method to form the same |
US10/680,618 US6924185B2 (en) | 2001-11-14 | 2003-10-07 | Fuse structure and method to form the same |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/992,344 Division US6927472B2 (en) | 2001-11-14 | 2001-11-14 | Fuse structure and method to form the same |
Publications (2)
Publication Number | Publication Date |
---|---|
US20040070049A1 US20040070049A1 (en) | 2004-04-15 |
US6924185B2 true US6924185B2 (en) | 2005-08-02 |
Family
ID=25538219
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/992,344 Expired - Fee Related US6927472B2 (en) | 2001-11-14 | 2001-11-14 | Fuse structure and method to form the same |
US10/680,618 Expired - Fee Related US6924185B2 (en) | 2001-11-14 | 2003-10-07 | Fuse structure and method to form the same |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/992,344 Expired - Fee Related US6927472B2 (en) | 2001-11-14 | 2001-11-14 | Fuse structure and method to form the same |
Country Status (1)
Country | Link |
---|---|
US (2) | US6927472B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090026574A1 (en) * | 2007-07-26 | 2009-01-29 | International Business Machines Corporation | Electrical fuse having sublithographic cavities thereupon |
US9059169B2 (en) | 2011-06-21 | 2015-06-16 | International Business Machines Corporation | E-fuse structures and methods of manufacture |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1450406A1 (en) * | 2003-02-19 | 2004-08-25 | Cavendish Kinetics Limited | Micro fuse |
TW200514235A (en) * | 2003-09-19 | 2005-04-16 | Koninkl Philips Electronics Nv | Fuse structure having reduced heat dissipation towards the substrate |
US7323761B2 (en) * | 2004-11-12 | 2008-01-29 | International Business Machines Corporation | Antifuse structure having an integrated heating element |
DE102005004108B4 (en) * | 2005-01-28 | 2007-04-12 | Infineon Technologies Ag | Semiconductor circuit and arrangement and method for controlling the fuse elements of a semiconductor circuit |
JP4959267B2 (en) * | 2006-03-07 | 2012-06-20 | ルネサスエレクトロニクス株式会社 | Method for increasing resistance value of semiconductor device and electric fuse |
US7566593B2 (en) * | 2006-10-03 | 2009-07-28 | International Business Machines Corporation | Fuse structure including cavity and methods for fabrication thereof |
US7741721B2 (en) * | 2007-07-31 | 2010-06-22 | International Business Machines Corporation | Electrical fuses and resistors having sublithographic dimensions |
JP5149576B2 (en) * | 2007-09-21 | 2013-02-20 | パナソニック株式会社 | Semiconductor device |
US7713792B2 (en) | 2007-10-10 | 2010-05-11 | International Business Machines Corporation | Fuse structure including monocrystalline semiconductor material layer and gap |
US9716064B2 (en) | 2015-08-14 | 2017-07-25 | International Business Machines Corporation | Electrical fuse and/or resistor structures |
CN109786364A (en) * | 2017-11-14 | 2019-05-21 | 中芯国际集成电路制造(上海)有限公司 | Fusing structure and forming method thereof |
US10910308B2 (en) * | 2018-05-09 | 2021-02-02 | Globalfoundries U.S. Inc. | Dual thickness fuse structures |
US11049681B1 (en) * | 2020-04-02 | 2021-06-29 | Littelfuse, Inc. | Protection device with u-shaped fuse element |
Citations (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4198744A (en) | 1978-08-16 | 1980-04-22 | Harris Corporation | Process for fabrication of fuse and interconnects |
US4491860A (en) | 1982-04-23 | 1985-01-01 | Signetics Corporation | TiW2 N Fusible links in semiconductor integrated circuits |
US4498068A (en) | 1982-12-13 | 1985-02-05 | Mcgraw-Edison Company | Magnetic arc extinguished fusible elements |
FR2575864A1 (en) | 1985-01-08 | 1986-07-11 | Nozick Jacques | Short-circuiting device for surge arrester |
US4679310A (en) | 1985-10-31 | 1987-07-14 | Advanced Micro Devices, Inc. | Method of making improved metal silicide fuse for integrated circuit structure |
US4796075A (en) | 1983-12-21 | 1989-01-03 | Advanced Micro Devices, Inc. | Fusible link structure for integrated circuits |
US4931353A (en) | 1989-03-01 | 1990-06-05 | The Boeing Company | Structure and method for selectively producing a conductive region on a substrate |
US5196819A (en) | 1991-02-28 | 1993-03-23 | Rock Ltd. Partnership | Printed circuits containing fuse elements and the method of making this circuit |
US5244836A (en) | 1991-12-30 | 1993-09-14 | North American Philips Corporation | Method of manufacturing fusible links in semiconductor devices |
US5451811A (en) | 1991-10-08 | 1995-09-19 | Aptix Corporation | Electrically programmable interconnect element for integrated circuits |
US5523253A (en) | 1994-03-31 | 1996-06-04 | International Business Machines Corp. | Array protection devices and fabrication method |
US5712206A (en) * | 1996-03-20 | 1998-01-27 | Vanguard International Semiconductor Corporation | Method of forming moisture barrier layers for integrated circuit applications |
US5757060A (en) | 1994-05-31 | 1998-05-26 | Taiwan Semiconductor Manufacturing Company, Ltd. | Contamination guard ring for semiconductor integrated circuit applications |
US5780918A (en) | 1990-05-22 | 1998-07-14 | Seiko Epson Corporation | Semiconductor integrated circuit device having a programmable adjusting element in the form of a fuse mounted on a margin of the device and a method of manufacturing the same |
US5882998A (en) | 1996-12-27 | 1999-03-16 | Vlsi Technology, Inc. | Low power programmable fuse structures and methods for making the same |
US5903041A (en) | 1994-06-21 | 1999-05-11 | Aptix Corporation | Integrated two-terminal fuse-antifuse and fuse and integrated two-terminal fuse-antifuse structures incorporating an air gap |
DE19803605A1 (en) | 1998-01-30 | 1999-08-05 | Wickmann Werke Gmbh | Electrical fuse element manufacturing method |
US6055150A (en) | 1996-05-02 | 2000-04-25 | Applied Materials, Inc. | Multi-electrode electrostatic chuck having fuses in hollow cavities |
US6117730A (en) * | 1999-10-25 | 2000-09-12 | Advanced Micro Devices, Inc. | Integrated method by using high temperature oxide for top oxide and periphery gate oxide |
JP2000299381A (en) * | 1999-04-16 | 2000-10-24 | Nec Corp | Semiconductor device and manufacturing method |
US6143642A (en) | 1997-12-22 | 2000-11-07 | Vlsi Technology, Inc. | Programmable semiconductor structures and methods for making the same |
WO2001017026A1 (en) * | 1999-09-01 | 2001-03-08 | International Business Machines Corporation | Post-fuse blow corrosion prevention structure for copper fuses |
US6242789B1 (en) * | 1999-02-23 | 2001-06-05 | Infineon Technologies North America Corp. | Vertical fuse and method of fabrication |
JP2001223272A (en) | 2000-02-09 | 2001-08-17 | Nec Corp | Semiconductor device |
US20020101324A1 (en) | 2001-01-31 | 2002-08-01 | Nippon Seisen Cable, Ltd. | Electric fuse |
US20020113291A1 (en) | 2001-02-16 | 2002-08-22 | International Business Machines Corporation | Fuse structure with thermal and crack-stop protection |
US20020132446A1 (en) * | 2001-03-02 | 2002-09-19 | Advanced Micro Devices | Process for fabricating a non-volatile memory device |
US20020142569A1 (en) * | 2001-03-29 | 2002-10-03 | Chang Kent Kuohua | Method for fabricating a nitride read-only -memory (nrom) |
US6495426B1 (en) | 2001-08-09 | 2002-12-17 | Lsi Logic Corporation | Method for simultaneous formation of integrated capacitor and fuse |
US6495901B2 (en) | 2001-01-30 | 2002-12-17 | Infineon Technologies Ag | Multi-level fuse structure |
US20030060036A1 (en) * | 2001-09-26 | 2003-03-27 | Hsu Sheng Teng | Method of fabricating copper interconnects with very low-k inter-level insulator |
US6680519B2 (en) * | 1998-01-29 | 2004-01-20 | Micron Technology, Inc. | Integrated circuitry fuse forming methods, integrated circuitry programming methods, and related integrated circuitry |
US6686644B2 (en) * | 2001-04-24 | 2004-02-03 | Fujitsu Limited | Semiconductor device provided with fuse and method of disconnecting fuse |
US20040046212A1 (en) * | 2001-02-07 | 2004-03-11 | Fujitsu Limited | Semiconductor memory capable of being driven at low voltage and its manufacture method |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH03124047A (en) * | 1989-10-06 | 1991-05-27 | Nec Ic Microcomput Syst Ltd | Integrated circuit device |
JPH03270255A (en) * | 1990-03-20 | 1991-12-02 | Fujitsu Ltd | Semiconductor device and its manufacture |
US5360988A (en) * | 1991-06-27 | 1994-11-01 | Hitachi, Ltd. | Semiconductor integrated circuit device and methods for production thereof |
SE469304B (en) * | 1991-11-18 | 1993-06-14 | Asea Brown Boveri | PROCEDURE FOR PRODUCING A POWER CIRCUIT |
JP3498919B2 (en) * | 1993-05-14 | 2004-02-23 | 清川メッキ工業株式会社 | Metal film resistor having fuse function and method of manufacturing the same |
US5751537A (en) * | 1996-05-02 | 1998-05-12 | Applied Materials, Inc. | Multielectrode electrostatic chuck with fuses |
JPH1131446A (en) * | 1997-07-11 | 1999-02-02 | Yazaki Corp | Device for detecting abnormality of wire harness for vehicle, and power source supplying device for vehicle |
JP3186664B2 (en) * | 1997-09-19 | 2001-07-11 | 日本電気株式会社 | Semiconductor device and method of manufacturing the same |
US6160302A (en) | 1998-08-31 | 2000-12-12 | International Business Machines Corporation | Laser fusible link |
JP4287543B2 (en) * | 1998-12-22 | 2009-07-01 | 矢崎総業株式会社 | Electrical circuit safety device and manufacturing method thereof |
US6633055B2 (en) * | 1999-04-30 | 2003-10-14 | International Business Machines Corporation | Electronic fuse structure and method of manufacturing |
-
2001
- 2001-11-14 US US09/992,344 patent/US6927472B2/en not_active Expired - Fee Related
-
2003
- 2003-10-07 US US10/680,618 patent/US6924185B2/en not_active Expired - Fee Related
Patent Citations (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4198744A (en) | 1978-08-16 | 1980-04-22 | Harris Corporation | Process for fabrication of fuse and interconnects |
US4491860A (en) | 1982-04-23 | 1985-01-01 | Signetics Corporation | TiW2 N Fusible links in semiconductor integrated circuits |
US4498068A (en) | 1982-12-13 | 1985-02-05 | Mcgraw-Edison Company | Magnetic arc extinguished fusible elements |
US4796075A (en) | 1983-12-21 | 1989-01-03 | Advanced Micro Devices, Inc. | Fusible link structure for integrated circuits |
FR2575864A1 (en) | 1985-01-08 | 1986-07-11 | Nozick Jacques | Short-circuiting device for surge arrester |
US4679310A (en) | 1985-10-31 | 1987-07-14 | Advanced Micro Devices, Inc. | Method of making improved metal silicide fuse for integrated circuit structure |
US4931353A (en) | 1989-03-01 | 1990-06-05 | The Boeing Company | Structure and method for selectively producing a conductive region on a substrate |
US5780918A (en) | 1990-05-22 | 1998-07-14 | Seiko Epson Corporation | Semiconductor integrated circuit device having a programmable adjusting element in the form of a fuse mounted on a margin of the device and a method of manufacturing the same |
US5196819A (en) | 1991-02-28 | 1993-03-23 | Rock Ltd. Partnership | Printed circuits containing fuse elements and the method of making this circuit |
US5451811A (en) | 1991-10-08 | 1995-09-19 | Aptix Corporation | Electrically programmable interconnect element for integrated circuits |
US5244836A (en) | 1991-12-30 | 1993-09-14 | North American Philips Corporation | Method of manufacturing fusible links in semiconductor devices |
US5523253A (en) | 1994-03-31 | 1996-06-04 | International Business Machines Corp. | Array protection devices and fabrication method |
US5757060A (en) | 1994-05-31 | 1998-05-26 | Taiwan Semiconductor Manufacturing Company, Ltd. | Contamination guard ring for semiconductor integrated circuit applications |
US5903041A (en) | 1994-06-21 | 1999-05-11 | Aptix Corporation | Integrated two-terminal fuse-antifuse and fuse and integrated two-terminal fuse-antifuse structures incorporating an air gap |
US5712206A (en) * | 1996-03-20 | 1998-01-27 | Vanguard International Semiconductor Corporation | Method of forming moisture barrier layers for integrated circuit applications |
US6055150A (en) | 1996-05-02 | 2000-04-25 | Applied Materials, Inc. | Multi-electrode electrostatic chuck having fuses in hollow cavities |
US5882998A (en) | 1996-12-27 | 1999-03-16 | Vlsi Technology, Inc. | Low power programmable fuse structures and methods for making the same |
US6143642A (en) | 1997-12-22 | 2000-11-07 | Vlsi Technology, Inc. | Programmable semiconductor structures and methods for making the same |
US6680519B2 (en) * | 1998-01-29 | 2004-01-20 | Micron Technology, Inc. | Integrated circuitry fuse forming methods, integrated circuitry programming methods, and related integrated circuitry |
DE19803605A1 (en) | 1998-01-30 | 1999-08-05 | Wickmann Werke Gmbh | Electrical fuse element manufacturing method |
US6242789B1 (en) * | 1999-02-23 | 2001-06-05 | Infineon Technologies North America Corp. | Vertical fuse and method of fabrication |
JP2000299381A (en) * | 1999-04-16 | 2000-10-24 | Nec Corp | Semiconductor device and manufacturing method |
US6300232B1 (en) * | 1999-04-16 | 2001-10-09 | Nec Corporation | Semiconductor device having protective films surrounding a fuse and method of manufacturing thereof |
US20030116820A1 (en) * | 1999-09-01 | 2003-06-26 | Daubenspeck Timothy H. | Post-fuse blow corrosion prevention structure for copper fuses |
WO2001017026A1 (en) * | 1999-09-01 | 2001-03-08 | International Business Machines Corporation | Post-fuse blow corrosion prevention structure for copper fuses |
US6117730A (en) * | 1999-10-25 | 2000-09-12 | Advanced Micro Devices, Inc. | Integrated method by using high temperature oxide for top oxide and periphery gate oxide |
JP2001223272A (en) | 2000-02-09 | 2001-08-17 | Nec Corp | Semiconductor device |
US6495901B2 (en) | 2001-01-30 | 2002-12-17 | Infineon Technologies Ag | Multi-level fuse structure |
US20020101324A1 (en) | 2001-01-31 | 2002-08-01 | Nippon Seisen Cable, Ltd. | Electric fuse |
US20040046212A1 (en) * | 2001-02-07 | 2004-03-11 | Fujitsu Limited | Semiconductor memory capable of being driven at low voltage and its manufacture method |
US20020113291A1 (en) | 2001-02-16 | 2002-08-22 | International Business Machines Corporation | Fuse structure with thermal and crack-stop protection |
US20020132446A1 (en) * | 2001-03-02 | 2002-09-19 | Advanced Micro Devices | Process for fabricating a non-volatile memory device |
US20020142569A1 (en) * | 2001-03-29 | 2002-10-03 | Chang Kent Kuohua | Method for fabricating a nitride read-only -memory (nrom) |
US6686644B2 (en) * | 2001-04-24 | 2004-02-03 | Fujitsu Limited | Semiconductor device provided with fuse and method of disconnecting fuse |
US6495426B1 (en) | 2001-08-09 | 2002-12-17 | Lsi Logic Corporation | Method for simultaneous formation of integrated capacitor and fuse |
US20030060036A1 (en) * | 2001-09-26 | 2003-03-27 | Hsu Sheng Teng | Method of fabricating copper interconnects with very low-k inter-level insulator |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090026574A1 (en) * | 2007-07-26 | 2009-01-29 | International Business Machines Corporation | Electrical fuse having sublithographic cavities thereupon |
US20100005649A1 (en) * | 2007-07-26 | 2010-01-14 | International Business Machines Corporation | Electrical fuse having sublithographic cavities thereupon |
US7675137B2 (en) | 2007-07-26 | 2010-03-09 | International Business Machines Corporation | Electrical fuse having sublithographic cavities thereupon |
US7785937B2 (en) | 2007-07-26 | 2010-08-31 | International Business Machines Corporation | Electrical fuse having sublithographic cavities thereupon |
US9059169B2 (en) | 2011-06-21 | 2015-06-16 | International Business Machines Corporation | E-fuse structures and methods of manufacture |
US9142506B2 (en) | 2011-06-21 | 2015-09-22 | International Business Machines Corporation | E-fuse structures and methods of manufacture |
Also Published As
Publication number | Publication date |
---|---|
US20030089962A1 (en) | 2003-05-15 |
US6927472B2 (en) | 2005-08-09 |
US20040070049A1 (en) | 2004-04-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6924185B2 (en) | Fuse structure and method to form the same | |
US6166423A (en) | Integrated circuit having a via and a capacitor | |
USRE36893E (en) | Anti-fuse structure for reducing contamination of the anti-fuse material | |
US6081021A (en) | Conductor-insulator-conductor structure | |
US6147404A (en) | Dual barrier and conductor deposition in a dual damascene process for semiconductors | |
US6251710B1 (en) | Method of making a dual damascene anti-fuse with via before wire | |
US6096648A (en) | Copper/low dielectric interconnect formation with reduced electromigration | |
JP5758344B2 (en) | System and method for bonding on active integrated circuits | |
US6468906B1 (en) | Passivation of copper interconnect surfaces with a passivating metal layer | |
US6124194A (en) | Method of fabrication of anti-fuse integrated with dual damascene process | |
US6355555B1 (en) | Method of fabricating copper-based semiconductor devices using a sacrificial dielectric layer | |
TW515099B (en) | Stacked structure for parallel capacitors and method of fabrication | |
US20120248567A1 (en) | Layered structure with fuse | |
EP1399958A1 (en) | Process for forming fusible links | |
CN1316589C (en) | Locally increasing sidewall density by ion implantation | |
US20100013045A1 (en) | Method of Integrating an Element | |
US6362526B1 (en) | Alloy barrier layers for semiconductors | |
US5639684A (en) | Method of making a low capacitance antifuse having a pillar located between the first and second metal layers | |
US6380003B1 (en) | Damascene anti-fuse with slot via | |
US6380625B2 (en) | Semiconductor interconnect barrier and manufacturing method thereof | |
US20050112957A1 (en) | Partial inter-locking metal contact structure for semiconductor devices and method of manufacture | |
US6251772B1 (en) | Dielectric adhesion enhancement in damascene process for semiconductors | |
US6107185A (en) | Conductive material adhesion enhancement in damascene process for semiconductors | |
WO2002041391A2 (en) | Amorphized barrier layer for integrated circuit interconnects | |
EP1943679A1 (en) | High density, high q capacitor on top of protective layer |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FEPP | Fee payment procedure |
Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
|
REMI | Maintenance fee reminder mailed | ||
LAPS | Lapse for failure to pay maintenance fees | ||
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
|
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20090802 |